-
公开(公告)号：US20150361827A1
公开(公告)日：2015-12-17
申请号：US14760746
申请日：2014-02-12
IPC分类号： F01D25/14
CPC分类号： F01D25/14 , F01D11/24 , F02C7/12 , F02C7/16 , F02C7/18 , F05D2250/182 , F05D2250/184
摘要： A cooling manifold has a plurality of pieces. The pieces extend in a circumferential direction to abutting flanges. The flanges are secured together at circumferential ends of each piece. Cooling channels are formed in between inner and outer walls. Air inlets are formed in the pieces with the air inlets delivering air in the interior. There are fingers on an outer periphery. The fingers are aligned within an air outlet. The air can be delivered into the inlet, cool the interior, and leave through the outlet extending to a main conduit. The main conduit is secured directly to an outer periphery of the cooling manifold.
摘要翻译： 冷却歧管具有多个部件。 这些件在圆周方向上延伸到邻接凸缘。 凸缘在每个件的圆周端固定在一起。 冷却通道形成在内壁和外壁之间。 空气入口形成在碎片中，空气入口在内部传送空气。 外周有手指。 手指在空气出口内对齐。 空气可以输送到入口，冷却内部，并通过出口延伸到主管道。 主导管直接固定在冷却歧管的外周。
-
公开(公告)号：US20140196434A1
公开(公告)日：2014-07-17
申请号：US13706445
申请日：2012-12-06
IPC分类号： F02C7/28
摘要： A system has a surface intended to separate two chambers within the system. The surface has an aperture for allowing passage of at least one communication conduit. A shroud is positioned on the surface at the aperture, and has at least two portions defining a central opening to allow the communication conduit to pass through the aperture and shroud. The two portions of shroud have mating clamp ears in contact with each other. Securement members tighten the clamp ears against each other to provide a seal at an end of the shroud remote from the surface.
摘要翻译： 系统具有旨在分离系统内的两个室的表面。 表面具有用于允许至少一个连通导管通过的孔。 护罩位于孔的表面上，并且具有限定中心开口的至少两个部分，以允许连通导管穿过孔和护罩。 护罩的两部分具有彼此接触的配合夹耳。 固定构件将夹紧耳紧紧地彼此紧固，以在远离表面的护罩的端部处提供密封。
-
公开(公告)号：US20200018427A1
公开(公告)日：2020-01-16
申请号：US16036628
申请日：2018-07-16
摘要： A mounting assembly for restricting movement of an electrical harness of a gas turbine engine includes a base, a first channel formed in the base and extending between a first surface and a second surface of the base, and a second channel formed in the base and extending between the first surface and a third surface of the base. The second surface and the third surface are distinct. At least one flexible connector is receivable within the first channel and the second channel. At least a portion of the at least one flexible connector extends about the electrical harness to couple the electrical harness to the base.
-
公开(公告)号：US09988943B2
公开(公告)日：2018-06-05
申请号：US14696615
申请日：2015-04-27
发明人： James P. Chasse, Jr. , Ryan K. Snyder , William K. Ackermann , Pellegrino J. Pisacreta , Judith F. Brooks , Stephanie Ernst
CPC分类号： F01D25/28 , F01D25/12 , F01D25/14 , F02C7/18 , Y02T50/675
摘要： A fitting according to an exemplary aspect of the present disclosure includes, among other things, a main body portion having a first axial end and a second axial end opposite the first axial end, an inlet provided at the first axial end, and an outlet adjacent the second axial end. The outlet includes a plurality of circumferentially spaced-apart slots formed through the main body portion, and each slot has an area within a range of 0.52 and 0.59 square inches.
-
公开(公告)号：US10934937B2
公开(公告)日：2021-03-02
申请号：US15213491
申请日：2016-07-19
摘要： A cooling system for an aircraft has at least one moveable member configured to cover an opening formed within an aircraft outer skin. An actuator moves the at least one moveable member between a fully open position where external atmosphere air can be directed through the opening to an internal passage enclosed by the aircraft outer skin and a fully closed position where the opening is covered. A controller selectively controls the actuator to move the at least one moveable member between the fully open and fully closed positions. An aircraft engine and a method of cooling an aircraft engine in an aircraft are also disclosed.
-
公开(公告)号：US10072520B2
公开(公告)日：2018-09-11
申请号：US14760746
申请日：2014-02-12
CPC分类号： F01D25/14 , F01D11/24 , F02C7/12 , F02C7/16 , F02C7/18 , F05D2250/182 , F05D2250/184
摘要： A cooling manifold has a plurality of pieces. The pieces extend in a circumferential direction to abutting flanges. The flanges are secured together at circumferential ends of each piece. Cooling channels are formed in between inner and outer walls. Air inlets are formed in the pieces with the air inlets delivering air in the interior. There are fingers on an outer periphery. The fingers are aligned within an air outlet. The air can be delivered into the inlet, cool the interior, and leave through the outlet extending to a main conduit. The main conduit is secured directly to an outer periphery of the cooling manifold.
-
公开(公告)号：US20160312660A1
公开(公告)日：2016-10-27
申请号：US14696615
申请日：2015-04-27
发明人： James P. Chasse, JR. , Ryan K. Snyder , William K. Ackermann , Pellegrino J. Pisacreta , Judith F. Brooks , Stephanie Ernst
CPC分类号： F01D25/28 , F01D25/12 , F01D25/14 , F02C7/18 , Y02T50/675
摘要： A fitting according to an exemplary aspect of the present disclosure includes, among other things, a main body portion having a first axial end and a second axial end opposite the first axial end, an inlet provided at the first axial end, and an outlet adjacent the second axial end. The outlet includes a plurality of circumferentially spaced-apart slots formed through the main body portion, and each slot has an area within a range of 0.52 and 0.59 square inches.
摘要翻译： 根据本公开的示例性方面的配件包括主体部分，其具有第一轴向端部和与第一轴向端部相对的第二轴向端部，设置在第一轴向端部处的入口和邻近的出口 第二个轴向端。 出口包括穿过主体部分形成的多个周向间隔开的槽，并且每个槽具有在0.52和0.59平方英寸的范围内的面积。
-
公开(公告)号：US10690267B2
公开(公告)日：2020-06-23
申请号：US16036628
申请日：2018-07-16
摘要： A mounting assembly for restricting movement of an electrical harness of a gas turbine engine includes a base, a first channel formed in the base and extending between a first surface and a second surface of the base, and a second channel formed in the base and extending between the first surface and a third surface of the base. The second surface and the third surface are distinct. At least one flexible connector is receivable within the first channel and the second channel. At least a portion of the at least one flexible connector extends about the electrical harness to couple the electrical harness to the base.
-
公开(公告)号：US20180022466A1
公开(公告)日：2018-01-25
申请号：US15213491
申请日：2016-07-19
CPC分类号： F02C7/141 , B64D33/08 , F02C7/18 , F02K1/825 , Y02T50/675
摘要： A cooling system for an aircraft has at least one moveable member configured to cover an opening formed within an aircraft outer skin. An actuator moves the at least one moveable member between a fully open position where external atmosphere air can be directed through the opening to an internal passage enclosed by the aircraft outer skin and a fully closed position where the opening is covered. A controller selectively controls the actuator to move the at least one moveable member between the fully open and fully closed positions. An aircraft engine and a method of cooling an aircraft engine in an aircraft are also disclosed.
-
公开(公告)号：US09835091B2
公开(公告)日：2017-12-05
申请号：US13706445
申请日：2012-12-06
摘要： A system has a surface intended to separate two chambers within the system. The surface has an aperture for allowing passage of at least one communication conduit. A shroud is positioned on the surface at the aperture, and has at least two portions defining a central opening to allow the communication conduit to pass through the aperture and shroud. The two portions of shroud have mating clamp ears in contact with each other. Securement members tighten the clamp ears against each other to provide a seal at an end of the shroud remote from the surface.
-
-
-
-
-
-
-
-
-
搜索结果
13 条记录 (耗时 0.013 秒)
